1NONLINEAR VIBRATIONS OF A ROLLING BEARING-ROTOR SYSTEM SUBJECT TO PARAMETRICAL AND EXTERNAL EXCITATIONSVibration·Noise·Monitoring·Diagnosis871-875
2STUDY OF FULL INFORMATION WAVELET ENERGY ENTROPY AND ITS APPLICATION IN ROTATING MACHINE CONDITION MONITORINGVibration·Noise·Monitoring·Diagnosis876-880
3STUDY ON STATE OBSERVER METHOD OF NONLINEAR CRACKED ROTOR SEAL CHAOTIC SYSTEMVibration·Noise·Monitoring·Diagnosis881-886
4STUDY ON STIFFNESS CONTRIBUTION OF SEPARATE TYPE BODY TO WHOLE FRAME-BODY STRUCTUREVibration·Noise·Monitoring·Diagnosis887-891
5NEW DYNAMIC MODEL OF THE 3D SQUEEZE FILM SYSTEM WITH A FLOATING RINGVibration·Noise·Monitoring·Diagnosis892-895
6FINITE ELEMENT ANALYSIS OF RANDOM VIBRATION RESPONSES FOR MULTILAYER SHELL STRUCTURE APPLIED WITH COMBINED TEMPERATURE AND VIBRATION ENVIRONMENTVibration·Noise·Monitoring·Diagnosis896-899
7BLIND SEPARATION METHOD BASED ON SECOND-ORDER STATISTICAL FOR CONVOLUTIVE MIXTURES OF NON-STATIONARY MECHANICAL VIBRATION SIGNALVibration·Noise·Monitoring·Diagnosis900-904
9EXPERIMENTAL STUDY ON CREEP-RECOVERY MECHANICAL BEHAVIOR OF ANISOTROPIC CONDUCTIVE ADHESIVESExperimental Research910-913
10RESEARCH OF MICRO-SPRINGS FORCE SENSOR FOR MICRO-TENSILE SYSTEMMicro-Electro-Mechanical System914-918
11TWO POINT EXPONENTIAL APPROXIMATION METHOD FOR STRUCTURAL RELIABILITY INDEX COMPUTATIONOptimization·Reliability919-925
12RELIABILITY SENSITIVITY DESIGN FOR MECHANICAL COMPONENTS WITH MULTI-FAILURE MODESOptimization·Reliability926-931
13STUDY OF THE DYNAMIC CRUSHING BEHAVIOR OF CELLULAR MATERIALS BY USING THE VORONOI RANDOM MODELSDesign·Calculation932-938
14STRESS AND STIFFNESS ANALYSIS OF A SIMPLIFIED ADHESIVE BONDED FINITE ELEMENT MODEL CONSIDERING SPEW-FILLETSDesign·Calculation939-946
15NUMERICAL ANALYSIS FOR TEMPERATURE FIELD OF ORTHOGONAL CUTTING UNDER DIFFERENT CONDITIONSDesign·Calculation947-951
16ESTABLISHMENT AND ANALYSIS OF SUCKER RODS MECHANICAL MODEL IN HORIZONTAL WELLDesign·Calculation952-956
18STUDY OF STRUCTURAL STABILITY DESIGN METHOD FOR BIG AIRPLANE STIFFENED PANELDesign·Calculation962-966
19DAMAGE ASSESSMENT OF HELICOPTER BLADE BASED ON CANTILEVER BEAM DISPLACEMENT MODELFatigue·Damage·Fracture·Failure Analysis967-971
20LOW CYCLE FATIGUE CRACK GROWTH RATE IN H2S ENVIRONMENTSFatigue·Damage·Fracture·Failure Analysis972-978
